Paper derives equations governing performance of ramjet using detonative combustion, and evaluates performance; engine layout permits normal detonation wave stabilized in diverging combustion chamber passage, or oblique wave stabilized on wedge; lower speed limit of detonative ramjet and cycle calculation; difficulties encountered by ramjets designed for hypersonic speeds may be alleviated if ramjet is designed to burn incoming air at supersonic velocities in stabilized detonation wave. (See also SAE -- Paper 419A for meeting Oct 9-13 1961 8 p)


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    Title :

    Performance of hypersonic ramjet using detonative combustion


    Additional title:

    SAE -- J


    Contributors:
    Arens, M. (author)


    Publication date :

    1961


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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